Numerical simulation of flow past an 8:1 oscillating rectangular cylinder at Re=22000

IF 1.3 4区 工程技术 Q3 MECHANICS Fluid Dynamics Research Pub Date : 2023-09-25 DOI:10.1088/1873-7005/acf8ee
Jian Wu, Yakun Liu, Di Zhang, Ze Cao
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Abstract

Abstract To investigate the influence of structure’s oscillatory motion on flow, the present study employs the arbitrary Lagrangian–Eulerian method in k – ω shear stress transport (SST) turbulence model to simulate the flow past an oscillating rectangular cylinder at Re = 22 000. The cylinder undergoes reciprocating sinusoidal motion at a specified frequency f e , and the frequency ratio fr (defined as the ratio of cylinder oscillation frequency f e to the stationary cylinder vortex shedding frequency f 0 ), ranges from 0 to 4. The results demonstrate that, in the synchronization region (0.8 ⩽ fr ⩽ 1.2), the drag coefficient shows the most notable variation and reaches its maxima at fr = 1.1 and the root mean square ( r.m.s. ) of the lift coefficient is proportional to the square of fr ( C l = 1.08 f r 2 , R 2 = 0.99). Moreover, the present study compares the similarities and differences of vortex shedding morphology between stationary and oscillating cylinders. With the increase of fr , the wake vortex gradually transforms from a single-row arrangement on the wake centerline to a parallel double-row arrangement, with the main vortex modes in the wake region observed as ‘2S’, ‘P + S’, ‘2P’ and ‘C’. Furthermore, spectral analysis, including amplitude spectrum analysis and wavelet analysis, in addition to probability density function statistical methods, are employed to comprehensively understand the velocity characteristics of the wake region. The results indicate that the oscillation of the cylinder reduces the correlation of the wake velocity. Those are beneficial in understanding the interaction between turbulence and structural fluid-induced motion.
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Re=22000时8:1振荡矩形圆柱流动的数值模拟
摘要为了研究结构振荡运动对流动的影响,本文采用k - ω剪切应力输运(SST)湍流模型中的任意拉格朗日-欧拉方法模拟了Re = 22 000处振荡矩形圆柱体的流动。气缸在指定频率fe下进行往复正弦运动,频率比fr(定义为气缸振荡频率fe与静止气缸涡流脱落频率f0之比)取值范围为0 ~ 4。结果表明,在同步区域(0.8≤fr≤1.2),阻力系数变化最为显著,在fr = 1.1和均方根(rms)时阻力系数达到最大值。升力系数的大小与fr的平方成正比(c1′= 1.08 * f r2, r2 = 0.99)。此外,本研究还比较了静止和振荡圆柱体的涡脱落形态的异同。随着流速的增加,尾流涡逐渐由尾流中心线上的单排排列转变为平行的双排排列,尾流区域的主要涡型为“2S”、“P + S”、“2P”和“C”。通过谱分析,包括幅谱分析和小波分析,以及概率密度函数统计方法,全面了解尾迹区域的速度特性。结果表明,圆柱的振荡降低了尾流速度的相关性。这有助于理解湍流和结构流体诱导运动之间的相互作用。
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来源期刊
Fluid Dynamics Research
Fluid Dynamics Research 物理-力学
CiteScore
2.90
自引率
6.70%
发文量
37
审稿时长
5 months
期刊介绍: Fluid Dynamics Research publishes original and creative works in all fields of fluid dynamics. The scope includes theoretical, numerical and experimental studies that contribute to the fundamental understanding and/or application of fluid phenomena.
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